US8449191B2 - Bearing structure, motor, and fan apparatus - Google Patents
Bearing structure, motor, and fan apparatus Download PDFInfo
- Publication number
- US8449191B2 US8449191B2 US12/542,065 US54206509A US8449191B2 US 8449191 B2 US8449191 B2 US 8449191B2 US 54206509 A US54206509 A US 54206509A US 8449191 B2 US8449191 B2 US 8449191B2
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- Prior art keywords
- sleeve
- ribs
- rotating shaft
- rib
- length
- Prior art date
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- Expired - Fee Related, expires
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
- F16C35/02—Rigid support of bearing units; Housings, e.g. caps, covers in the case of sliding-contact bearings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/06—Units comprising pumps and their driving means the pump being electrically driven
- F04D25/0606—Units comprising pumps and their driving means the pump being electrically driven the electric motor being specially adapted for integration in the pump
- F04D25/0613—Units comprising pumps and their driving means the pump being electrically driven the electric motor being specially adapted for integration in the pump the electric motor being of the inside-out type, i.e. the rotor is arranged radially outside a central stator
- F04D25/062—Details of the bearings
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/05—Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
- F04D29/056—Bearings
- F04D29/057—Bearings hydrostatic; hydrodynamic
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/10—Construction relative to lubrication
- F16C33/1025—Construction relative to lubrication with liquid, e.g. oil, as lubricant
- F16C33/103—Construction relative to lubrication with liquid, e.g. oil, as lubricant retained in or near the bearing
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K5/00—Casings; Enclosures; Supports
- H02K5/04—Casings or enclosures characterised by the shape, form or construction thereof
- H02K5/16—Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields
- H02K5/167—Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields using sliding-contact or spherical cap bearings
- H02K5/1675—Means for supporting bearings, e.g. insulating supports or means for fitting bearings in the bearing-shields using sliding-contact or spherical cap bearings radially supporting the rotary shaft at only one end of the rotor
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2360/00—Engines or pumps
- F16C2360/46—Fans, e.g. ventilators
Definitions
- the present invention relates to a bearing structure, a motor, and a fan apparatus.
- a plurality of ribs extending in an axial direction are typically provided on an inner surface of a cavity portion of a sleeve support portion arranged to support a sleeve having a rotating shaft inserted therein.
- the ribs press the sleeve, which is press fitted within the sleeve support portion, radially inward to retain the sleeve.
- Such bearing structures have some disadvantages.
- the pressing force applied by the ribs of the sleeve support portion onto the sleeve is too small, the positioning of the sleeve and the rotating shaft may become so insufficient that a problem, such as sway of the rotating shaft, may occur.
- the pressing force applied by the ribs of the sleeve support portion onto the sleeve is too large, the sleeve may be excessively compressed by the pressing force from the ribs such that the sleeve may be deformed, resulting in a failure to support the rotating shaft stably.
- the optimum amount of the pressing force to be applied by the ribs onto the sleeve varies at different axial positions on the sleeve.
- an axial center of gravity of a rotating body including the rotating shaft is sometimes located in that portion of the cavity portion of the sleeve support portion which is located toward an opening portion, in an axial direction of the sleeve. Therefore, more careful control of the amount of the pressing force applied by the ribs onto the sleeve is required for that portion of the cavity portion than for the other portions.
- a bearing structure including a rotating shaft; a sleeve being substantially tubular and having the rotating shaft inserted therein such that the rotating shaft is rotatable; a sleeve support portion having a bottom and being substantially tubular, extending in an axial direction, and arranged to support the sleeve; and a base portion connected to an axial end of the sleeve support portion.
- the sleeve support portion preferably includes an opening portion arranged to receive the rotating shaft; a cavity portion being continuous with the opening portion and arranged to contain the sleeve; and a plurality of ribs provided on an inner surface of the cavity portion and extending in the axial direction, the ribs being spaced from each other in a circumferential direction centered on the rotating shaft.
- Each of the ribs includes a contact surface arranged to make contact with at least a portion of an outer surface of the sleeve.
- the ribs are preferably defined by a plurality of types of ribs, each type of the ribs being different in an axial position of an axial edge of the contact surface on an axially opening portion side.
- a bearing structure preferably including a rotating shaft; a sleeve being substantially tubular and having the rotating shaft inserted therein such that the rotating shaft is rotatable; a sleeve support portion having a bottom and being substantially tubular, extending in an axial direction, and arranged to support the sleeve; and a base portion connected to an axial end of the sleeve support portion.
- the sleeve support portion preferably includes an opening portion arranged to receive the rotating shaft; a cavity portion being continuous with the opening portion and arranged to contain the sleeve; and a plurality of ribs provided on an inner surface of the cavity portion and extending in the axial direction, the ribs being spaced from each other in a circumferential direction centered on the rotating shaft, and arranged to make contact with at least a portion of the sleeve.
- Each of the ribs includes an opposed surface raised toward an outer surface of the sleeve relative to the inner surface of the cavity portion, and opposed to the outer surface of the sleeve.
- At least one of the ribs is a varied projection dimension rib, in which a radial distance between the opposed surface and a shaft center of the rotating shaft varies with respect to the axial direction in at least a partial section of an entire length thereof along the axial direction.
- a bearing structure including a rotating shaft; a sleeve being substantially tubular and having the rotating shaft inserted therein such that the rotating shaft is rotatable; a sleeve support portion having a bottom and being substantially tubular, extending in an axial direction, and arranged to support the sleeve; and a base portion connected to an axial end of the sleeve support portion.
- the sleeve support portion preferably includes an opening portion arranged to receive the rotating shaft; a cavity portion being continuous with the opening portion and arranged to contain the sleeve; and a plurality of ribs provided on an inner surface of the cavity portion and extending in the axial direction, the ribs being spaced from each other in a circumferential direction centered on the rotating shaft, and arranged to make contact with at least a portion of an outer surface of the sleeve.
- At least one of the ribs is a varied width rib, whose width in the circumferential direction varies with respect to the axial direction in at least a partial section of an entire length thereof along the axial direction.
- a plurality of ribs including the contact surface arranged to make contact with at least a portion of the outer surface of the sleeve are provided on the inner surface of the cavity portion of the sleeve support portion, and the ribs are preferably defined by a plurality of types of ribs, each type of the ribs being different in the axial position of the axial edge of the contact surface on the axially opening portion side.
- the number of ribs that make contact with the sleeve can be reduced to easily optimize the amount of pressing force applied by the ribs onto the sleeve for that portion of the sleeve which is located toward the axially opening portion side so that an appropriate reduction in the pressing force can be achieved to reduce deformation of the sleeve (e.g., to prevent an excessive reduction in inside diameter of the sleeve).
- a greater number of ribs are arranged to make contact with a remaining portion of the sleeve which is located on the opposite side to the axially opening portion side, as compared to the number of ribs arranged to make contact with that portion of the sleeve which is located toward the axially opening portion side. This contributes to pressing the sleeve securely so as to ensure stable support of the sleeve, while reducing the deformation of the sleeve caused by circumferential variations in the pressing force applied by the ribs onto the sleeve.
- FIG. 1 is a cross-sectional view of a fan apparatus to which a bearing structure according to a first preferred embodiment of the present invention is applied.
- FIG. 2 is a cross-sectional view of a sleeve support portion provided in the fan apparatus as illustrated in FIG. 1 .
- FIG. 3 is a plan view of the sleeve support portion as illustrated in FIG. 2 , as viewed from above in an axial direction.
- FIG. 4 is a diagram illustrating a variation of the structure of the sleeve support portion as illustrated in FIG. 3 .
- FIG. 5 is a cross-sectional view of a sleeve support portion provided in a fan apparatus to which a bearing structure according to a second preferred embodiment of the present invention is applied.
- FIG. 6 is a diagram illustrating a variation of the structure of the sleeve support portion as illustrated in FIG. 5 .
- FIGS. 7A and 7B are diagrams of a varied width rib and a uniform width rib, respectively, which are provided on a sleeve support portion of a fan apparatus to which a bearing structure according to a third preferred embodiment of the present invention is applied, as viewed radially from the direction of a rotating shaft.
- FIGS. 8A , 8 B, and 8 C are diagrams illustrating variations of the varied width rib as illustrated in FIG. 7A .
- a fan apparatus 1 preferably includes an impeller 2 , a motor 3 , a circuit board 4 , a base portion 5 , a sleeve 6 , a sleeve support portion 7 , a plurality of stationary vanes 8 , and an outer frame portion 9 .
- the impeller 2 preferably includes a plurality of rotor blades 21 , a rotor blade support portion 22 , and a rotating shaft 23 .
- the motor 3 preferably includes an armature 31 , which is a stationary motor component; and a rotor magnet 32 and a rotor holder 33 , all of which are rotating motor components.
- the impeller 2 , the rotor magnet 32 , and the rotor holder 33 form parts of the rotating body 10 .
- the side where the impeller 2 is arranged and the side where the stationary vanes 8 are arranged, along an axial direction A of the rotating shaft 23 are assumed to be an upper side and a lower side, respectively.
- the axial direction A may not necessarily coincide with the direction of gravity.
- the rotor blade support portion 22 is preferably substantially cup-shaped, and arranged to surround the motor 3 .
- the rotor blades 21 which extend radially outward, are provided on an outer surface of the rotor blade support portion 22 .
- the rotor blades 21 are preferably arranged at regular intervals in a circumferential direction.
- the rotor holder 33 which is preferably made of metal and substantially cylindrical, is provided on an inner surface of the rotor blade support portion 22 .
- the rotor magnet 32 which is substantially cylindrical, is fixed to an inner circumferential surface of the rotor holder 33 by, for example, press fitting, via an adhesive, or any other suitable attachment method.
- the rotating shaft 23 is located substantially in the center of the rotor blade support portion 22 , and is provided integrally with the rotor blades 21 , the rotor blade support portion 22 , and the rotor holder 33 by injection molding, for example.
- Grooves are preferably formed by knurling or the like, for example, on an outer surface of a top portion (with respect to the axial direction A) of the rotating shaft 23 .
- resin flows into the grooves, so that the rotating shaft 23 and the rotor blade support portion 22 are firmly coupled with each other.
- the armature 31 of the motor 3 is supported by the base portion 5 as described below.
- the armature 31 and the rotor magnet 32 are arranged radially opposite to each other.
- the circuit board 4 which is positioned below the armature 31 with respect to the axial direction A, is fixed to the base portion 5 , and electrically connected to the armature 31 via conductive pins or the like, for example.
- the circuit board 4 includes a circuit designed to control current supplied to the motor 3 , and is electrically connected to an external power supply (not shown) via a lead wire (not shown) or the like.
- the base portion 5 has a bottom, is substantially cylindrical, is positioned radially inward of the outer frame portion 9 , and is arranged to support the armature 31 of the motor 3 and the circuit board 4 . Moreover, a lower end (with respect to the axial direction A) of the sleeve support portion 7 is connected to the base portion 5 .
- the structures of the sleeve 6 and the sleeve support portion 7 will be described in detail below.
- the stationary vanes 8 are arranged upstream or downstream of the rotor blades 21 of the impeller 2 with respect to the flow of air generated by the rotation of the rotor blades 21 , and control the flow of air taken in or sent out by the rotor blades 21 .
- the stationary vanes 8 are arranged below the rotor blades 21 , downstream thereof, with respect to the axial direction A.
- the stationary vanes 8 are arranged at regular intervals in the circumferential direction between the outer frame portion 9 and the base portion 5 .
- the stationary vanes 8 have both ends thereof joined to the outer frame portion 9 and the base portion 5 , to support the base portion 5 .
- the outer frame portion 9 is arranged to surround the impeller 2 .
- the base portion 5 , the sleeve support portion 7 , the stationary vanes 8 , and the outer frame portion 9 may be formed integrally by molding using resin or metal (e.g., aluminum) to define a single continuous member, for example.
- resin or metal e.g., aluminum
- An example of a die applicable in this molding process is a type of mold that allows the mold to release in the axial direction A.
- the sleeve 6 is preferably substantially tubular (and in the present preferred embodiment, substantially cylindrical), and has the rotating shaft 23 inserted therein such that the rotating shaft is rotatable.
- the sleeve 6 is, for example, made of porous sintered metal obtained by heating and consolidating metal particles, and is impregnated with lubricating fluid such as oil. The lubricating fluid, exuding from the sleeve 6 , reduces friction between the sleeve 6 and the rotating shaft 23 .
- An upper small diameter portion 6 f , a lower small diameter portion 6 g , and an intermediate large diameter portion 6 h are provided on an inner surface 6 d of the sleeve 6 .
- a reduced diameter portion 6 e is defined at a lower end portion (with respect to the axial direction A) of an outer surface of the sleeve 6 .
- the upper small diameter portion 6 f and the lower small diameter portion 6 g which have substantially the same inside diameter, are provided at an upper end portion and a lower end portion (with respect to the axial direction A), respectively, of the inner surface 6 d of the sleeve 6 .
- the intermediate large diameter portion 6 h which has a larger inside diameter than those of the upper and lower small diameter portions 6 f and 6 g , is provided between the upper and lower small diameter portions 6 f and 6 g along the axial direction A.
- a suitable gap is secured between the intermediate large diameter portion 6 h and the rotating shaft 23 .
- a purpose of the provision of the intermediate large diameter portion 6 h is to reduce an area of contact between the inner surface 6 d of the sleeve 6 and the rotating shaft 23 , and thereby reduce frictional resistance.
- An additional purpose of the provision of the intermediate large diameter portion 6 h is to secure space to retain the lubricating fluid inside the sleeve 6 . Accordingly, in that portion of the sleeve 6 where the intermediate large diameter portion 6 h is provided, deformation of the inner surface 6 d of the sleeve 6 which might be caused by a pressing force applied by ribs 73 and 74 would be less likely to affect the support of the rotating shaft 23 .
- a substantially tubular object is first formed by, for example, powder pressing, and the upper small diameter portion 6 f and the intermediate large diameter portion 6 h are formed on the inner surface 6 d of the substantially tubular object.
- the lower small diameter portion 6 g has not been formed yet, and a portion corresponding to the lower small diameter portion 6 g has substantially the same inside diameter as that of the intermediate large diameter portion 6 h .
- the outer diameter of an outer surface of the substantially tubular object is substantially the same throughout the length thereof along the axial direction A. Then, this aggregate of solid particles obtained by the powder pressing is heated to form a sintered body of the above-described shape.
- a sizing bar having an outer diameter substantially the same as the inside diameter of the upper small diameter portion 6 f is inserted in the center of the sintered body. Further, the sintered body is subjected to press working such that a lower end portion (with respect to the axial direction A) of an outer surface of the sintered body is pressed against the sizing bar. As a result, the lower small diameter portion 6 g , whose inside diameter is substantially the same as the outer diameter of the sizing bar, is formed at a lower end portion (with respect to the axial direction A) on an inner surface of the sintered body.
- the reduced diameter portion 6 e which is smaller in outer diameter than an outer surface 6 a of the sleeve 6 , is formed at the lower end portion (with respect to the axial direction A) of the outer surface of the sintered body, as a result of the above-described press working.
- the sleeve support portion 7 extends along the axial direction A, has a bottom and is substantially tubular and thus surrounds and supports the sleeve 6 .
- the sleeve support portion 7 is provided with an opening portion 71 , a cavity portion 72 , and a plurality of ribs 73 and 74 .
- the opening portion 71 is provided at an upper end (with respect to the axial direction A) of the sleeve support portion 7 , and is arranged to receive the rotating shaft 23 and the sleeve 6 .
- an additional opening portion may be provided at a lower end (with respect to the axial direction A) of the sleeve support portion 7 .
- the sleeve 6 may be inserted through the additional opening portion at the lower end and, for example, press fit within the sleeve support portion 7 , and then the additional opening portion at the lower end may be closed.
- the cavity portion 72 is provided below the opening portion 71 with respect to the axial direction A, and is continuous with the opening portion 71 , and arranged to contain the sleeve 6 .
- an inner surface 72 a of the cavity portion 72 is substantially in the shape of a cylinder extending along the axial direction A.
- the plurality of ribs 73 and 74 are provided on the inner surface 72 a of the sleeve support portion 7 , and extend substantially in the axial direction A.
- the ribs 73 and 74 are arranged to be spaced from one another in a circumferential direction centered on the rotating shaft 23 .
- the ribs 73 and 74 have contact surfaces 73 a and 74 a which are arranged to make contact with at least a portion of the outer surface 6 a of the sleeve 6 .
- the contact surfaces 73 a and 74 a of the ribs 73 and 74 are in contact with the outer surface 6 a of the sleeve 6 so as to be pressed radially inward against the outer surface 6 a of the sleeve 6 .
- This allows the sleeve 6 to be positioned and held within the cavity portion 72 .
- both ends 6 b and 6 c (with respect to the axial direction A) of the sleeve 6 are located within the cavity portion 72 (see FIG. 1 ).
- a lower end (with respect to the axial direction A) of the rotating shaft 23 and the lower end 6 c (with respect to the axial direction A) of the sleeve 6 are located at a bottom of the cavity portion 72 , i.e., at a lower end (with respect to the axial direction A) of the cavity portion 72 .
- the ribs 73 and 74 as described above have edge positions 73 b and 74 b at edges of the contact surfaces 73 a and 74 a on a side (with respect to the axial direction A) where the opening portion 71 is provided (this side will be hereinafter referred to simply as an “axially opening portion side” as appropriate).
- the edge positions 73 b and 74 b have a plurality of positions, each of the positions being different with respect to the axial direction A.
- edge position 73 b of the contact surface 73 a of each of the greater-length ribs 73 is arranged closer to the axially opening portion side than the edge position 74 b of the contact surface 74 a of each of the shorter-length ribs 74 .
- Edge positions 73 c and 74 c of the contact surfaces 73 a and 74 a of the greater-length and shorter-length ribs 73 and 74 , on an opposite side to the axially opening portion side, are at substantially the same position with respect to the axial direction A.
- the edge positions 73 c and 74 c of the greater-length and shorter-length ribs 73 and 74 are located at a lower end (with respect to the axial direction A) of the cavity portion 72 , on the opposite side to the axially opening portion side. Note that, in the present preferred embodiment, the edge positions 73 c and 74 c substantially coincide with positions of ends of the ribs 73 and 74 on the opposite side to the axially opening portion side.
- the number of greater-length ribs 73 as described above is at least one (three in the present preferred embodiment), and the number of shorter-length ribs 74 is at least one (three in the present preferred embodiment) (see FIG. 3 ).
- the greater-length and shorter-length ribs 73 and 74 are arranged alternately and at regular intervals in the circumferential direction, and arranged to be axially symmetrical with respect to the shaft center 23 a.
- a center of gravity Bc of the rotating body 10 is either located at substantially the same axial position as an end 73 d or 74 d , on the axially opening portion side, of the rib 73 or 74 that is most on the axially opening portion side of all the plurality of ribs 73 and 74 , or located more on the cavity portion 72 side with respect to the axial direction A (this side will be hereinafter referred to as an “axially cavity portion side” as appropriate) than that end 73 d or 74 d .
- the center of gravity Bc of the rotating body 10 is either located at substantially the same axial position as the end 73 d of the greater-length ribs 73 on the axially opening portion side, or located more on the axially cavity portion side than that end 73 d .
- the center of gravity Bc of the rotating body 10 is located between the edge position 73 b of the contact surface 73 a of the greater-length ribs 73 and the edge position 74 b of the contact surface 74 a of the shorter-length ribs 74 with respect to the axial direction A.
- the end 6 b of the sleeve 6 on the axially opening portion side is located, with respect to the axial direction A, between the edge position 73 b of the contact surface 73 a of the greater-length ribs 73 and the edge position 74 b of the contact surface 74 a of the shorter-length ribs 74 .
- the center of gravity Bc of the rotating body 10 is located, with respect to the axial direction A, more on the axially cavity portion side than the end 6 b of the sleeve 6 on the axially opening portion side, but toward the axially opening portion side.
- the center of gravity Bc of the rotating body 10 is located in that portion of the sleeve 6 which is located toward the axially opening portion side. Therefore, the amount of the pressing force applied by the greater-length and shorter-length ribs 73 and 74 to that portion of the sleeve 6 which is located toward the axially opening portion side is a very important factor for stable support of the rotating shaft 23 .
- the contact surfaces 73 a and 74 a of the greater-length and shorter-length ribs 73 and 74 provided on the inner surface 72 a of the cavity portion 72 of the sleeve support portion 7 have different edge positions 73 b and 74 b with respect to the axial direction A, as described above.
- the center of gravity Bc of the rotating body 10 is located, with respect to the axial direction A, between the edge position 73 b of the contact surface 73 a of the greater-length ribs 73 and the edge position 74 b of the contact surface 74 a of the shorter-length ribs 74 .
- the reduced diameter portion 6 e is provided on the outer surface of the sleeve 6 , as described above. Neither the greater-length ribs 73 nor the shorter-length ribs 74 make contact with the reduced diameter portion 6 e . That is, each of the greater-length and shorter-length ribs 73 and 74 makes contact with only the other portions of the outer surface 6 a than the reduced diameter portion 6 e , so as to ensure a sufficient strength of the support of the sleeve 6 by the sleeve support portion 7 . Thus, the support strength increases as the number of ribs increases. In the present preferred embodiment, the combined total number of the greater-length and shorter-length ribs is six, but it should be noted that any desirable number of ribs could be provided.
- both the greater-length and shorter-length ribs 73 and 74 make contact with that portion of the outer surface 6 a which is located radially outward of the intermediate large diameter portion 6 h , so as to ensure sufficient support strength thereat.
- both the contact surfaces 73 a of the greater-length ribs 73 and the contact surfaces 74 a of the shorter-length ribs 74 make contact with that portion of the outer surface 6 a of the sleeve 6 which is located on the axially cavity portion side of both a portion thereof corresponding to the position of the center of gravity Bc of the rotating body 10 and a portion thereof corresponding to the upper small diameter portion 6 f .
- the number of ribs that press the sleeve 6 is greater, by the number of shorter-length ribs 74 , at that portion of the outer surface 6 a of the sleeve 6 which is located on the axially cavity portion side of both the portion thereof corresponding to the position of the center of gravity Bc of the rotating body 10 and the portion thereof corresponding to the upper small diameter portion 6 f than at the portion thereof corresponding to the upper small diameter portion 6 f .
- the greater-length ribs 73 apply necessary pressing force onto that portion of the sleeve 6 which is located toward the axially opening portion side and where the center of gravity Bc of the rotating body 10 is located, to position the sleeve 6 and ensure the stable support of the sleeve 6 .
- the greater-length and shorter-length ribs 73 and 74 are arranged alternately in the circumferential direction. Therefore, the pressing force applied by the greater-length ribs 73 onto that portion of the sleeve 6 which is located toward the axially opening portion side is well balanced with respect to the circumferential direction. Thus, the circumferential variations in the pressing force applied by the greater-length ribs 73 onto the sleeve 6 are reduced, so that the deformation of the sleeve 6 can be reduced.
- the greater-length and shorter-length ribs 73 and 74 are arranged to be axially symmetrical with respect to the shaft center 23 a . This allows the pressing force applied by the greater-length and shorter-length ribs 73 and 74 onto the sleeve 6 to be axially symmetrical with respect to the shaft center 23 a . This allows the sleeve 6 to be stably supported by the greater-length and shorter-length ribs 73 and 74 , and contributes to reducing the circumferential variations in the pressing force applied by the greater-length and shorter-length ribs 73 and 74 onto the sleeve 6 , to reduce the deformation of the sleeve 6 .
- both ends 6 b and 6 c of the sleeve 6 with respect to the axial direction A are located within the cavity portion 72 of the sleeve support portion 7 . Therefore, the majority of the entire length of the sleeve 6 along the axial direction A is pressed by the greater-length and shorter-length ribs 73 and 74 of the sleeve support portion 7 , to ensure the stable support of the sleeve 6 . Moreover, in the case where the lubricating fluid is used to reduce the friction between the sleeve 6 and the rotating shaft 23 , the lubricant is less likely to leak out from within the cavity portion 72 of the sleeve support portion 7 .
- a circumferential width W 1 of the greater-length ribs 73 is substantially equal to a circumferential width W 2 of the shorter-length ribs 74 .
- the circumferential widths W 1 and W 2 may have different values in other preferred embodiments of the present invention.
- a radial distance D 1 between the contact surface 73 a of the greater-length rib 73 and the shaft center 23 a and a radial distance D 2 between the contact surface 74 a of the shorter-length rib 74 and the shaft center 23 a are set at substantially the same value, before the sleeve 6 is, for example, press fitted within the sleeve support portion 7 .
- the radial distances D 1 and D 2 may be set at different values in other preferred embodiments of the present invention.
- both the number of greater-length ribs 73 and the number of shorter-length ribs 74 are three. Note, however, that both the number of greater-length ribs 73 and the number of shorter-length ribs 74 may be two or more than three in other preferred embodiments of the present invention. Also note that the number of greater-length ribs 73 and the number of shorter-length ribs 74 may be different in other preferred embodiments of the present invention.
- two types of ribs i.e., the greater-length ribs 73 and the shorter-length ribs 74 .
- three or more types of ribs may be provided, each type of ribs being different in the edge position of the contact surface on the axially opening portion side with respect to the axial direction A.
- three types of ribs 75 , 76 , and 77 are arranged at regular intervals in the circumferential direction so as to be axially symmetrical with respect to the shaft center 23 a .
- the edge position of the ribs 75 is located most on the axially opening portion side
- the edge position of the ribs 77 is located most on the axially cavity portion side
- the edge position of the ribs 76 is located at an intermediate position between them.
- FIG. 5 is a cross-sectional view of a sleeve support portion 7 provided in a fan apparatus 1 to which a bearing structure according to a second preferred embodiment of the present invention is applied.
- the fan apparatus 1 according to the present preferred embodiment is essentially identical to the fan apparatus 1 according to the first preferred embodiment except in the structure of ribs 171 and 172 . Accordingly, like portions are designated by like reference numerals and redundant description is omitted.
- At least one of the ribs 171 and 172 provided on the inner surface 72 a of the sleeve support portion 7 is not uniform in the radial dimension, i.e., in how far it projects from the inner surface 72 a of the sleeve support portion 7 toward the shaft center 23 a .
- This type of ribs will be referred to as “varied projection dimension ribs” as appropriate.
- a radial distance D 3 between the shaft center 23 a and an opposed surface 171 a of the varied projection dimension rib 171 , which is opposed to the outer surface 6 a of the sleeve 6 varies with respect to the axial direction A.
- At least one varied projection dimension rib 171 and at least one uniform projection dimension rib 172 are provided on the inner surface 72 a of the sleeve support portion 7 .
- a radial distance D 4 between the shaft center 23 a and an opposed surface 172 a of the uniform projection dimension rib 172 which is opposed to the outer surface 6 a of the sleeve 6 , is substantially uniform along an entire length of the uniform projection dimension rib 172 along the axial direction A.
- a plurality of (e.g., three) varied projection dimension ribs 171 and a plurality of (e.g., three) uniform projection dimension ribs 172 are arranged at regular intervals in the circumferential direction to be axially symmetrical with respect to the shaft center 23 a .
- all the ribs provided on the inner surface 72 a of the sleeve support portion 7 may be composed of varied projection dimension ribs 171 .
- Both ends 171 b and 171 c (with respect to the axial direction A) of the varied projection dimension rib 171 are located at substantially the same axial positions as both ends 172 b and 172 c , respectively, of the uniform projection dimension rib 172 .
- the end 171 c of the varied projection dimension rib 171 on the axially cavity portion side (i.e., on the lower side with respect to the axial direction A) and the end 172 c of the uniform projection dimension rib 172 on the axially cavity portion side (i.e., on the lower side with respect to the axial direction A) are located at the end of the cavity portion 72 on the axially cavity portion side (i.e., on the lower side with respect to the axial direction A).
- an enlarging section 171 d is provided at an end portion of the varied projection dimension rib 171 on the axially opening portion side.
- the distance D 3 between the opposed surface 171 a and the shaft center 23 a gradually increases toward the axially opening portion side.
- a uniform section 171 e is provided at that portion of the varied projection dimension rib 171 which is located on the axially cavity portion side of the enlarging section 171 d in the opposed surface 171 a .
- the enlarging section 171 d may extend over substantially the entire length of the opposed surface 171 a of the varied projection dimension rib 171 along the axial direction A.
- the sleeve 6 has a portion with which the enlarging section 171 d of the opposed surface 171 a of the varied projection dimension rib 171 makes contact.
- the amount of the pressing force applied by the opposed surface 171 a of the varied projection dimension rib 171 decreases toward the axially opening portion side.
- the center of gravity Bc of the rotating body 10 is located in that portion of the sleeve 6 which is located toward the axially opening portion side with respect to the axial direction A.
- the center of gravity Bc of the rotating body 10 is either located at substantially the same axial position as the ends 171 b and 172 b of the varied and uniform projection dimension ribs 171 and 172 on the axially opening portion side, or located more on the axially cavity portion side than the ends 171 b and 172 b .
- the enlarging section 171 d of the opposed surface 171 a of the varied projection dimension rib 171 substantially corresponds to that portion of the outer surface 6 a of the sleeve 6 where the center of gravity Bc of the rotating body 10 is located.
- the enlarging section 171 d of the opposed surface 171 a of the varied projection dimension rib 171 it is possible to allow the enlarging section 171 d of the opposed surface 171 a of the varied projection dimension rib 171 to correspond to an end portion of the outer surface 6 a of the sleeve 6 on the axially opening portion side where the upper small diameter portion 6 f is provided on the inner surface 6 d of the sleeve 6 .
- the uniform section 171 e of the opposed surface 171 a of the varied projection dimension rib 171 and the opposed surface 172 a of the uniform projection dimension rib 172 are arranged to make contact with that portion of the outer surface 6 a of the sleeve 6 which is located on the axially cavity portion side of that portion of the sleeve 6 where the center of gravity Bc of the rotating body 10 is located. This leads to an increase in the number of ribs 171 and 172 pressing the sleeve 6 , or in the area of contact.
- the use of the varied and uniform projection dimension ribs 171 and 172 contributes to partially reducing the pressing force applied onto that portion of the sleeve 6 which is located toward the axially opening portion side and which is concerned with problems such as the problem of the excessive reduction in the inside diameter of the sleeve 6 caused by the pressing force applied by the ribs 171 and 172 .
- the combined use of the varied and uniform projection dimension ribs 171 and 172 produces a beneficial effect as described below.
- the uniform projection dimension rib 172 in which the radial distance D 4 between the opposed surface 172 a and the shaft center 23 a is uniform with respect to the axial direction A, applies the pressing force to the sleeve 6 substantially uniformly with respect to the axial direction A. Therefore, the uniform projection dimension rib 172 supports each axial position of the sleeve 6 stably.
- the additional use of the varied projection dimension rib 171 allows optimization of the amount of the pressing force applied by the varied and uniform projection dimension ribs 171 and 172 to each axial position of the sleeve 6 .
- the varied and uniform projection dimension ribs 171 and 172 are arranged alternately in the circumferential direction. This contributes to preventing the addition of the varied projection dimension ribs 171 from causing uneven circumferential distribution of the pressing force applied by the varied and uniform projection dimension ribs 171 and 172 onto the sleeve 6 (this is especially true for that portion of the sleeve 6 which is located toward the axially opening portion side). This contributes to achieving the stable support of the sleeve 6 , while reducing the deformation of the sleeve 6 caused by the circumferential variations in the pressing force applied by the ribs 171 and 172 onto the sleeve 6 .
- the varied and uniform projection dimension ribs 171 and 172 are arranged to be axially symmetrical with respect to the shaft center 23 a . This allows the pressing force applied by the varied and uniform projection dimension ribs 171 and 172 onto the sleeve 6 to be axially symmetrical with respect to the shaft center 23 a . This allows the sleeve 6 to be stably supported by the varied and uniform projection dimension ribs 171 and 172 , and contributes to reducing the circumferential variations in the pressing force applied by the ribs 171 and 172 onto the sleeve 6 , to reduce the deformation of the sleeve 6 .
- an end 171 f , on the axially opening portion side, of the enlarging section 171 d of the opposed surface 171 a of the varied projection dimension rib 171 and a boundary portion 171 g between the enlarging section 171 d and the uniform section 171 e may be in the shape of a smooth curve in a section taken along the axial direction A.
- the opposed surface 171 a of the varied projection dimension rib 171 may be in various other shapes in section taken along the axial direction A, in other preferred embodiments of the present invention.
- FIGS. 7A and 7B are diagrams of a varied width rib 271 and a uniform width rib 272 , respectively, which are provided on a sleeve support portion 7 of a fan apparatus 1 to which a bearing structure according to a third preferred embodiment of the present invention is applied, as viewed radially from the direction of the rotating shaft 23 .
- the fan apparatus 1 according to the present preferred embodiment is essentially identical to the fan apparatus 1 according to the first preferred embodiment except in the structure of the varied and uniform width ribs 271 and 272 . Accordingly, like portions are designated by like reference numerals, and redundant description is omitted.
- At least one of the ribs 271 and 272 provided on the inner surface 72 a of the sleeve support portion 7 is not uniform in width.
- This type of ribs will be referred to as “varied width ribs” as appropriate.
- a width W 3 in a circumferential direction C centered on the shaft center 23 a varies with respect to the axial direction A.
- At least one varied width rib 271 and at least one uniform width rib 272 are provided on the inner surface 72 a of the sleeve support portion 7 .
- a width W 4 in the circumferential direction C is substantially uniform over its entire axial length.
- a plurality of (e.g., three) varied width ribs 271 and a plurality of (e.g., three) uniform width ribs 272 are arranged at regular intervals in the circumferential direction to be axially symmetrical with respect to the shaft center 23 a .
- all the ribs provided on the inner surface 72 a of the sleeve support portion 7 may be varied width ribs 271 .
- Both ends 271 b and 271 c (with respect to the axial direction A) of the varied width rib 271 are located at substantially the same axial positions as both ends 272 b and 272 c , respectively, of the uniform width rib 272 .
- the end 271 c of the varied width rib 271 on the axially cavity portion side (i.e., on the lower side with respect to the axial direction A) and the end 272 c of the uniform width rib 272 on the axially cavity portion side (i.e., on the lower side with respect to the axial direction A) are located at the end of the sleeve support portion 7 on the axially cavity portion side (i.e., on the lower side with respect to the axial direction A).
- a decreased width section 271 d is provided at an end portion of the varied width rib 271 on the axially opening portion side, while a uniform width section 271 e is provided to extend from an end of the decreased width section 271 d on the axially cavity portion side to the end of the varied width rib 271 on the axially cavity portion side.
- the width W 3 of the varied width rib 271 is smaller than the width W 3 of the varied width rib 271 in the uniform width section 271 e , and the width W 3 gradually decreases toward the axially opening portion side.
- the width W 3 of the varied width rib 271 is uniform with respect to the axial direction A.
- both side surfaces 271 f and 271 g , in the circumferential direction C, of the varied width rib 271 in the decreased width section 271 d may assume a tapered shape such that the width W 3 decreases substantially linearly toward the axially opening portion side.
- the side surfaces 271 f and 271 g may assume a curved shape such that the width W 3 decreases at an increasing rate toward the axially opening portion side.
- the width W 3 of the varied width rib 271 in the decreased width section 271 d may be uniform with respect to the axial direction A (but is smaller than the width W 3 in the uniform width section 271 e ).
- the width W 3 may gradually decrease toward the axially opening portion side over the entire axial length of the varied width rib 271 .
- both side surfaces, in the circumferential direction, of the varied width rib 271 may be laterally asymmetrical when viewed radially from the inside.
- the width W 3 of the varied width rib 271 is smaller in the decreased width section 271 d than in the uniform width section 271 e . Accordingly, the amount of the pressing force applied by a contact surface 271 a of the varied width rib 271 is smaller for that portion of the sleeve 6 which makes contact with the decreased width section 271 d of the varied width rib 271 than for that portion of the sleeve 6 which makes contact with the uniform width section 271 e .
- the width W 3 of the varied width rib 271 in the decreased width section 271 d gradually decreases toward the axially opening portion side; therefore, the amount of the pressing force applied by the varied width rib 271 becomes progressively smaller toward the axially opening portion side, for that portion of the sleeve 6 which makes contact with the decreased width section 271 d of the varied width rib 271 .
- the width W 4 is substantially uniform over its entire axial length, and accordingly, the amount of the pressing force applied by the uniform width rib 272 onto the sleeve 6 is substantially uniform with respect to the axial direction A.
- the center of gravity Bc of the rotating body 10 is, with respect to the axial direction A, located in that portion of the sleeve 6 which is located toward the axially opening portion side.
- the center of gravity Bc of the rotating body 10 is either located at substantially the same axial position as the ends 271 b and 272 b of the varied and uniform width ribs 271 and 272 on the axially opening portion side, or located more on the axially cavity portion side than the ends 271 b and 272 b .
- the decreased width section 271 d of the varied width rib 271 substantially corresponds to that portion of the outer surface 6 a of the sleeve 6 where the center of gravity Bc of the rotating body 10 is located.
- the decreased width section 271 d of the varied width rib 271 it is possible to allow the decreased width section 271 d of the varied width rib 271 to correspond to an end portion of the outer surface 6 a of the sleeve 6 on the axially opening portion side where the upper small diameter portion 6 f is provided on the inner surface 6 d of the sleeve 6 .
- the addition of the varied width rib 271 as described above allows an appropriate reduction in the radially inward pressing force applied onto that portion of the sleeve 6 which is located toward the axially opening portion side and where the center of gravity Bc of the rotating body 10 and the upper small diameter portion 6 f of the sleeve 6 are located, and facilitates the optimization of the amount of the pressing force applied by the ribs 271 and 272 so as to reduce the deformation of the sleeve 6 (e.g., to prevent an excessive reduction in the inside diameter of the sleeve 6 ).
- the total number of varied and uniform width ribs 271 and 272 can be set at a number that allows an effective reduction in the deformation of the sleeve 6 caused by circumferential variations in the pressing force applied by the ribs 271 and 272 .
- the decreased width section 271 d of the varied width rib 271 is arranged to substantially correspond to the outer surface 6 a of that portion of the sleeve 6 where the center of gravity Bc of the rotating body 10 and the upper small diameter portion 6 f of the sleeve 6 are located. This allows more effective control of the pressing force applied to that portion of the sleeve 6 .
- the uniform width section 271 e of the varied width rib 271 applies the pressing force substantially uniformly over the axial length of that portion of the sleeve 6 which makes contact with the uniform width section 271 e of the varied width rib 271 , to achieve the stable support of the sleeve 6 .
- the combined use of the varied and uniform width ribs 271 and 272 produces a beneficial effect as described below.
- the uniform width rib 272 whose width W 3 is uniform with respect to the axial direction A, applies the pressing force to the sleeve 6 substantially uniformly with respect to the axial direction A. Therefore, the uniform width rib 272 supports each axial position of the sleeve 6 stably.
- the additional use of the varied width rib 271 allows the optimization of the amount of the pressing force applied by the varied and uniform width ribs 271 and 272 to each axial position of the sleeve 6 .
- varied and uniform width ribs 271 and 272 are arranged alternately in the circumferential direction. This contributes to preventing the addition of the varied width ribs 271 from causing uneven circumferential distribution of the pressing force applied by the varied and uniform width ribs 271 and 272 onto the sleeve 6 (this is especially true for that portion of the sleeve 6 which is located toward the axially opening portion side). This contributes to achieving the stable support of the sleeve 6 , while reducing the deformation of the sleeve 6 caused by the circumferential variations in the pressing force applied by the ribs 271 and 272 onto the sleeve 6 .
- the varied and uniform width ribs 271 and 272 are preferably arranged to be substantially axially symmetrical with respect to the shaft center 23 a . This allows the pressing force applied by the varied and uniform width ribs 271 and 272 onto the sleeve 6 to be substantially axially symmetrical with respect to the shaft center 23 a . This allows the sleeve 6 to be stably supported by the varied and uniform width ribs 271 and 272 , and contributes to reducing the circumferential variations in the pressing force applied by the ribs 271 and 272 onto the sleeve 6 , to reduce the deformation of the sleeve 6 .
- the bearing structures according to the preferred embodiments are applied to the fan apparatus 1 .
- the bearing structures according to the preferred embodiments are applicable not only to the fan apparatus 1 but also to various other devices having a bearing structure. Examples of other applications include, for example, disc drive apparatuses designed to rotate a disc-shaped recording medium and any other devices that include electric motors.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Power Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Mounting Of Bearings Or Others (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
- Sliding-Contact Bearings (AREA)
Abstract
Description
Claims (10)
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
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JP2008-222466 | 2008-08-29 | ||
JP2008222466 | 2008-08-29 | ||
JP2009162471A JP5439991B2 (en) | 2008-08-29 | 2009-07-09 | Bearing structure, motor and fan device |
JP2009-162471 | 2009-07-09 |
Publications (2)
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US20100054965A1 US20100054965A1 (en) | 2010-03-04 |
US8449191B2 true US8449191B2 (en) | 2013-05-28 |
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US12/542,065 Expired - Fee Related US8449191B2 (en) | 2008-08-29 | 2009-08-17 | Bearing structure, motor, and fan apparatus |
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US (1) | US8449191B2 (en) |
JP (1) | JP5439991B2 (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101064456B1 (en) * | 2009-08-28 | 2011-09-15 | 엘지이노텍 주식회사 | Bearing structure and spindle motor |
KR101039635B1 (en) * | 2010-03-11 | 2011-06-08 | 주식회사 제이엠더블유 | BLC motor for hair dryer |
US10605248B2 (en) * | 2010-03-15 | 2020-03-31 | Ebm-Papst St. Georgen Gmbh & Co. Kg | External rotor motor with integrated bearing housing and box for control electronics |
CN118490942A (en) | 2011-04-18 | 2024-08-16 | 瑞思迈发动机及马达技术股份有限公司 | PAP system blower |
JP2013108470A (en) * | 2011-11-24 | 2013-06-06 | Nippon Densan Corp | Fan |
WO2013162122A1 (en) * | 2012-04-23 | 2013-10-31 | 주식회사 제이엠더블유 | Bldc motor having sintered bearings for hair dryer |
KR101309689B1 (en) * | 2012-11-29 | 2013-10-14 | 주식회사 한일파테크 | Bldc motor for electric device |
US9624929B2 (en) * | 2012-12-21 | 2017-04-18 | Lg Innotek Co., Ltd. | Electric pump |
JP2018178802A (en) * | 2017-04-07 | 2018-11-15 | 日本電産株式会社 | Fan motor |
WO2021125114A1 (en) * | 2019-12-17 | 2021-06-24 | アルプスアルパイン株式会社 | Lens driving device and camera module |
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Also Published As
Publication number | Publication date |
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JP2010078143A (en) | 2010-04-08 |
JP5439991B2 (en) | 2014-03-12 |
US20100054965A1 (en) | 2010-03-04 |
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